CTHIn ForceLegislation
AD/B737/359 - Outboard Landing Light Wire Bundles
Boeing 737 Series AeroplanesBoeing 737 Series Aeroplanes
Start here
Get a plain-English read of Boeing 737 Series Aeroplanes
Turn the raw legal text into a practical explanation grounded in AD/B737/359 - Outboard Landing Light Wire Bundles.
Boeing 737 Series Aeroplanes
| AD/B737/359 | Outboard Landing Light Wire Bundles | 9/2009 |
|---|
| Applicability: | Model 737-100, -200, -200C, -300, -400 and -500 series aeroplanes, as identified in Boeing Service Bulletin (SB) 737-28-1241, Revision 1, dated 31 August 2007. |
|---|---|
| Requirement: | 1. For Model 737-300, -400 and -500 series aeroplanes identified in Boeing Alert Service Bulletin (ASB) 737-33A1140, dated 22 May 2006 - Accomplish either of the following actions: |
| a. Deactivate the outboard landing lights by accomplishing all of theactions specified in Part 1 of the Accomplishment Instructions of ASB737-33A1140, or | |
| b. Modify the wiring to the outboard landing lights by accomplishing all of the actions specified in Part 2 of the Accomplishment Instructions of ASB737-33A1140. | |
| Note 1: The Master Minimum Equipment List (MMEL) prohibits dispatching an aeroplane for night operations with deactivated outboard landing lights in the event that either of the inboard landing lights fail. Operators should note that, if the outboard landing lights are deactivated in accordance with Part 1 of ASB737-33A1140 there is no MMEL relief allowing for this configuration for night operations should any inboard landing light fail. | |
| 2. For all aeroplanes - Accomplish following actions in accordance with737-28-1241, Revision 1: | |
| a. Replace the wire bundles for the landing lights and fuel shutoff valves with new, redesigned wire bundles and carry out the related investigative, other specified, together with corrective actions, as applicable. The related investigative, other specified and corrective actions must be done before further flight after the replacement. | |
| b. Carry out detailed inspection for any broken, damaged, or missing fairleads, any damaged or missing grommets and any chafed or damaged wires or wire bundles in the four electrical junction boxes of the main wheel well, and do the applicable corrective actions. The corrective actions must be done before further flight after the inspection. |
| c. Replace the electrical connectors and backshell clamps with new, improved electrical connectors and backshell clamps, as applicable. |
|---|